REG NASA-LLIS-5183-2012 Flight Termination System (FTS) Safe and Arm (S&A) Device Monitoring Capability.pdf

上传人:dealItalian200 文档编号:1019485 上传时间:2019-03-21 格式:PDF 页数:2 大小:57.72KB
下载 相关 举报
REG NASA-LLIS-5183-2012 Flight Termination System (FTS) Safe and Arm (S&A) Device Monitoring Capability.pdf_第1页
第1页 / 共2页
REG NASA-LLIS-5183-2012 Flight Termination System (FTS) Safe and Arm (S&A) Device Monitoring Capability.pdf_第2页
第2页 / 共2页
亲,该文档总共2页,全部预览完了,如果喜欢就下载吧!
资源描述

1、Public Lessons Learned Entry: 5183 Lesson Info: Lesson Number: 5183 Submitting Organization: KSC Submitted by: Jenni Palmer Subject: Flight Termination System (FTS) Safe and Arm (S&A) Device Monitoring Capability Abstract: Late in the Constellation Program, a trade study was performed to assess ordn

2、ance connects and closeouts in the Vehicle Assembly Building (VAB) at the Kennedy Space Center. This trade study discussed the need for ground system upgrades in the processing flow. One of these upgrades required establishing a monitoring capability for a Flight Termination System (FTS) Safe and Ar

3、m (S&A) device when power is removed during vehicle rollout. This operational upgrade will require process modification to ground and flight subsystems. Description of Driving Event: A trade study to evaluate closeout for vehicle ordnance access while in the VAB was approved by the Operations Contro

4、l Panel/Program Review Board (OCP/PRB). Lesson(s) Learned: Safety concluded that S&A monitoring may be required continuously during vehicle rollout if ordnance is connected. Acquiring this capability would require that existing ground systems and flight avionics hardware be upgraded. Recommendation(

5、s): If ordnance is to be connected to a launch vehicle and power is to be disconnected from the vehicle in an off-pad integration facility, then design and installation work for new ground and flight system components will be necessary to set up monitoring of an FTS S&A device. A requirement for thi

6、s upgrade should be added to both project and subsystem ground and flight elements. Evidence of Recurrence Control Effectiveness: N/A Documents Related to Lesson: N/A Mission Directorate(s): Exploration Systems Additional Key Phrase(s): Systems Engineering and Analysis. Systems Engineering and Analy

7、sis.Level II/III requirements definition Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Additional Info: Project: Constellation Approval Info: Approval Date: 2012-08-22 Approval Name: mbell Approval Organization: HQ Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-

展开阅读全文
相关资源
猜你喜欢
  • EN 2815-2009 en Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Bar for machining - a or D Less tha.pdf EN 2815-2009 en Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Bar for machining - a or D Less tha.pdf
  • EN 2817-2009 en Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Bar for machining - a or D Less tha.pdf EN 2817-2009 en Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Bar for machining - a or D Less tha.pdf
  • EN 2818-2009 en Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D Less than or equa.pdf EN 2818-2009 en Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D Less than or equa.pdf
  • EN 2821-2007 en Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Bar for machining - a or D or = to .pdf EN 2821-2007 en Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Bar for machining - a or D or = to .pdf
  • EN 2823-2017 en Aerospace series - Fibre reinforced plastics - Determination of the effect of exposure to humid atmosphere on physical and mechanical characteristics《航空航天系列-纤维增强塑料-.pdf EN 2823-2017 en Aerospace series - Fibre reinforced plastics - Determination of the effect of exposure to humid atmosphere on physical and mechanical characteristics《航空航天系列-纤维增强塑料-.pdf
  • EN 2824-2011 en Aerospace series - Burning behaviour of non-metallic materials under the influence of radiating heat and flames - Determination of smoke density and gas components .pdf EN 2824-2011 en Aerospace series - Burning behaviour of non-metallic materials under the influence of radiating heat and flames - Determination of smoke density and gas components .pdf
  • EN 2825-2011 en Aerospace series - Burning behaviour of non metallic materials under the influence of radiating heat and flames - Determination of smoke density《航空航天系列 辐射热和火焰的影响下的非.pdf EN 2825-2011 en Aerospace series - Burning behaviour of non metallic materials under the influence of radiating heat and flames - Determination of smoke density《航空航天系列 辐射热和火焰的影响下的非.pdf
  • EN 2826-2011 en Aerospace series - Burning behaviour of non metallic materials under the influence of radiating heat and flames - Determination of gas components in the smoke《航空航天系.pdf EN 2826-2011 en Aerospace series - Burning behaviour of non metallic materials under the influence of radiating heat and flames - Determination of gas components in the smoke《航空航天系.pdf
  • EN 2828-1993 en Aerospace Series - Adhesion Test for Metallic Coatings by Burnishing《航空航天系列 通过压光法检验金属镀层的粘附强度》.pdf EN 2828-1993 en Aerospace Series - Adhesion Test for Metallic Coatings by Burnishing《航空航天系列 通过压光法检验金属镀层的粘附强度》.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > 其他

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1